TY - GEN
T1 - Research on an Adaptive Ice Tolerance Control Method for Aircraft
AU - Jiang, Feihong
AU - Li, Kecheng
AU - Chen, Tongwen
AU - Liu, Xiaoxiong
N1 - Publisher Copyright:
© The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2025.
PY - 2025
Y1 - 2025
N2 - In order to effectively address the impact of icing on flight control performance, this paper proposes an ice tolerance adaptive flight control method. By combining projection operator technology, an adaptive law for model reference adaptive control is designed to address the deficiency of losing control robustness due to changes of aircraft aerodynamic derivatives under icing conditions, and the stability of the proposed projection operator adaptive control is demonstrated. On this basis, an aircraft angular rate loop control law is designed based on the projection operator model reference adaptive control method. The designed control law is simulated and verified under the circumstances of icing environment, according to the aerodynamic parameter disturbances. The simulation results show that the designed projection operator adaptive control law can overcome the influence of icing on the aircraft aerodynamic and control characteristics, ensuring that the tracking error quickly converges to zero.
AB - In order to effectively address the impact of icing on flight control performance, this paper proposes an ice tolerance adaptive flight control method. By combining projection operator technology, an adaptive law for model reference adaptive control is designed to address the deficiency of losing control robustness due to changes of aircraft aerodynamic derivatives under icing conditions, and the stability of the proposed projection operator adaptive control is demonstrated. On this basis, an aircraft angular rate loop control law is designed based on the projection operator model reference adaptive control method. The designed control law is simulated and verified under the circumstances of icing environment, according to the aerodynamic parameter disturbances. The simulation results show that the designed projection operator adaptive control law can overcome the influence of icing on the aircraft aerodynamic and control characteristics, ensuring that the tracking error quickly converges to zero.
KW - Model reference adaptive control
KW - fault-tolerant control
KW - ice tolerance adaptive flight control
UR - http://www.scopus.com/inward/record.url?scp=86000479850&partnerID=8YFLogxK
U2 - 10.1007/978-981-96-2252-8_12
DO - 10.1007/978-981-96-2252-8_12
M3 - 会议稿件
AN - SCOPUS:86000479850
SN - 9789819622511
T3 - Lecture Notes in Electrical Engineering
SP - 115
EP - 124
BT - Advances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control
A2 - Yan, Liang
A2 - Duan, Haibin
A2 - Deng, Yimin
PB - Springer Science and Business Media Deutschland GmbH
T2 - International Conference on Guidance, Navigation and Control, ICGNC 2024
Y2 - 9 August 2024 through 11 August 2024
ER -